Terminal structure of high-pressure fuel pipe for direct injection engine

ABSTRACT

Provided is a terminal structure of a high-pressure fuel pipe for a direct injection engine which can prevent stress concentration to a brazed portion between a pipe and a connection part effectively. In the terminal structure of a high-pressure fuel pipe for a direct injection engine where a connection head is brazed to an end of a fuel pipe, the end of the fuel pipe continued to a fuel pipe insertion portion of the connection head is provided with a drawn portion, an outer diameter D 1  of the drawn portion to a fuel pipe diameter D satisfies 0.8D≦D 1 ≦0.9D, and a length L 1  of the drawn portion having the outer diameter D 1  in a pipe-axial direction from an end of the fuel pipe insertion portion satisfies L 1 ≧0.06D.

The present application is a divisional application of U.S. patentapplication Ser. No. 14/380,512, filed Aug. 22, 2014, the contents ofwhich are hereby incorporated by reference in their entirety.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to one used in a high-pressure fuelpassage connecting between a high-pressure fuel pump and a fuel rail ina fuel supplying apparatus for a direct injection engine, and morespecifically relates to a terminal structure of a high-pressure fuelpipe for a direct injection engine where a connection head is brazed toan end of a fuel pipe composed of a steel pipe or a stainless steelpipe.

2. Description of the related Art

As a conventional terminal structure of a high-pressure fuel pipe for adirect injection engine, there is generally one where a connection headhaving a spherical or a curved-face pressing seat face and a fuel pipeinsertion portion positioned on the opposite side of the pressing seatface is brazed to an end of a fuel pipe composed of a steel pipe or astainless steel pipe.

FIG. 5 shows an example of the terminal structure of a high-pressurefuel pipe for a direct injection engine, and one where a connection head22 having a spherical or a curved-face pressing seat face 22-1 at adistal end thereof and a fuel pipe insertion portion 22-2 (generallycalled “hakama (skirt)” in Japan) for securing a brazing area on theopposite side of the pressing seat face has been brazed to an end of afuel pipe 21 composed of a steel pipe or a stainless pipe is known (seeDE 10 2005 045 731 A1). That is, such a terminal structure of ahigh-pressure fuel pipe for a direct injection engine is configured byfitting the fuel pipe insertion portion 22-2 of the connection head 22having a spherical or a curved-face pressing seat face 22-1 at a distalend thereof and the fuel pipe insertion portion 22-2 formed on theopposite side of the pressing seat face to a straight pipe portion atthe end of the fuel pipe 21 composed of a steel pipe or a stainlesssteel pipe and brazing the fitted portion.

Further, FIG. 6 shows an example of a terminal structure of an eye jointused for a high-pressure fuel pipe for a direct injection engine, wherean eye joint main body (corresponding to the above “connection head”) 24having an annular recessed groove 24-1 internally, having a wall portion24-2 positioned on the side of a circumferential side of the annularrecessed groove 24-1 and bulged in an arc shape, having a connectionhole 24-3 communicating with the annular recessed groove 24-1 and amounting hole 24-4 bored at an axial core portion, and having a shortcylindrical wall (corresponding to the above “hakama”) 24-5 formed byintegrally protruding a hole peripheral wall of the connection hole 24-3outward and having an inner diameter smaller than a diameter of the fuelpipe 23 has been brazed to an end of a fuel pipe 23 composed of a steelpipe or a stainless steel pipe, and this eye joint is configured byperforming one-stage drawing work to the connection end of the fuel pipe23, fitting the drawn portion into the short cylindrical wall 24-5 ofthe eye joint main body and brazing the fitted portion (see JapanesePatent Application Laid-Open No. H1992-347091).

However, such conventional terminal structures of a high-pressure fuelpipe for a direct injection engine and of the eye joint used for ahigh-pressure fuel pipe for a direct injection engine have the followingproblems described below.

In the case of the terminal structure of a high-pressure fuel pipe for adirect injection engine shown in FIG. 5, by providing the fuel pipeinsertion portion (hakama) 22-2 for securing a brazing area on theopposite side of the pressing seat face 22-1 of the connection head 22,such an effect that enables to secure a sufficient brazing area andthereby a brazing strength to the connection head 22 to improve can beachieved; however, since the straight pipe portion of the end of thefuel pipe 21 is fitted to the fuel pipe insertion portion (hakama) 22-2of the connection head 22 to be brazed, a thinner pipe must be adoptedas the fuel pipe 21, which results in such a problem that an innervolume cannot be secured sufficiently and requirements cannot besatisfied regarding such a performance aspect as pulsation or pressureloss.

Further, in the terminal structure of an eye joint used for ahigh-pressure fuel pipe for a direct injection engine shown in FIG. 6,since the eye joint is configured by performing one-stage drawing workto the straight pipe portion at the end of the fuel pipe 23 to reduce adiameter of the straight pipe portion, fitting the reduced-diameter pipeportion into the short cylindrical wall 24-5 of the eye joint main body24, and brazing the fitted portion, there is such a problem that stressis concentrated to the drawn portion of the terminal portion of the fuelpipe 23 in the vicinity of the short cylindrical wall 24-5 and apossibility that the fuel pipe 23 is broken from the drawn portionbecomes large.

The present invention has been made in order to solve such conventionalproblems, and an object thereof is to propose a terminal structure of ahigh-pressure fuel pipe for a direct injection engine which not only canimprove the brazing strength to the connection head but also can preventstress concentration to the brazed portion with the connection headeffectively even if a thin-diameter pipe is adopted as the fuel pipe anddrawing work has been applied to an end of the pipe in view of theproblem of pulsation or an internal volume, the performance aspect, orthe like.

SUMMARY OF THE INVENTION

A terminal structure of a high-pressure fuel pipe for a direct injectionengine according to the present invention is one of a high-pressure fuelpipe for a direct injection engine where a connection head is brazed toan end of a fuel pipe composed of a steel pipe or a stainless pipe, theconnection head having a spherical or a curved-face pressing seat faceat a distal end thereof and a fuel pipe insertion portion on theopposite side of the pressing seat face; wherein the end of the fuelpipe continued to the fuel pipe insertion portion of the connection headis provided with a one-stage drawn portion, an outer diameter D1 of thedrawn portion relative to a fuel pipe diameter D satisfying 0.8 D≦D1≦0.9D; and wherein a length L1 of the drawn portion having the outerdiameter D1 from an end of the fuel pipe insertion portion in an axialdirection of the pipe satisfies L1≧0.06 D.

Further, another terminal structure of a high-pressure fuel pipe for adirect injection engine according to the present invention is one of ahigh-pressure fuel pipe for a direct injection engine, where aconnection head is brazed to an end of a fuel pipe composed of a steelpipe or a stainless pipe, the connection head having a spherical or acurved-face pressing seat face at a distal end thereof and a fuel pipeinsertion portion on the opposite side of the pressing seat face;wherein the end of the fuel pipe continued to the fuel pipe insertionportion of the connection head has a two-stage drawn portion, an outerdiameter D1 of a first-stage drawn portion located on the side of theconnection head, relative to a fuel pipe diameter D, satisfying0.8≦D1≦0.9 D; wherein a length L1 of the first-stage drawn portionhaving the outer diameter D1 from an end of the fuel pipe insertionportion in an axial direction of the pipe satisfies L1≧0.06 D; andwherein a second-stage drawn portion continued to the first-stage drawnportion has a straight pipe portion having an outer diameter D2 largerthan the outer diameter D1 of the first-stage drawn portion.

Additionally, the present invention includes a preferred aspect where alinear length L2 in the axial direction of the pipe from a terminal end,on the opposite side to the connection head, of the length L1 of thedrawn portion having the outer diameter D1 in the axial direction of thepipe, to a drawing-termination end, is 0.14 D or more, and an entirelength (L1+L2) of the drawn portion of the pipe is 1.5 D or less.

The present invention is the terminal structure of a high-pressure fuelpipe for a direct injection engine where a connection head having aspherical or a curved-face pressing seat face at a distal end of theconnection head and a fuel pipe insertion portion on the opposite sideof the pressing seat face is brazed to an end of a fuel pipe composed ofa steel pipe or a stainless pipe, wherein a one-stage drawn portion isformed at the end of the fuel pipe continued to the fuel pipe insertionportion of the connection head; an outer diameter D1 of the drawnportion to a fuel pipe diameter D satisfies 0.8≦D1≦0.9 D; and a lengthL1 of the drawn portion having the outer diameter D1 in an axialdirection of the pipe from an end of the fuel pipe insertion portion hasa straight pipe portion satisfying L1 0.06 D, and at the result, stressconcentration to a brazed portion with the connection head can beprevented effectively. Further, in another terminal structure where atwo-stage drawn portion is formed at the end of the fuel pipe continuedto the fuel pipe insertion portion of the connection head, a first-stagedrawn portion located on the side of the connection head has an outerdiameter D1 to a fuel pipe diameter D satisfying 0.8≦D1≦0.9 D in asimilar manner as the above; a straight pipe portion satisfying acondition where a length L1 of the first-stage drawn portion having theouter diameter D1 in an axial direction of the pipe from an end of thefuel pipe insertion portion has a straight pipe portion satisfyingL1≧0.06 D; and a second-stage drawn portion continued to the first-stagedrawn portion has a straight pipe portion having an outer diameter D2larger than the outer diameter D1 of the first-stage drawn portion, andat the result, a dispersion effect of stress acting on the fuel pipe canbe obtained, so that even if a load (displacement) in a bendingdirection to the high-pressure fuel pipe occurs, stress concentration isavoided and the problem of breaking of a fuel pipe is almost solved.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a sectional view showing an example of a terminal structure ofa high-pressure fuel pipe for a direction injection engine according tothe present invention;

FIG. 2 is a sectional view showing another example of the terminalstructure of a high-pressure fuel pipe for a direction injection enginelike the above;

FIG. 3 is a graph showing a relationship between a bending stress and anouter diameter ratio in Example 1 of the present invention;

FIG. 4 is a graph showing a relationship between increase of pressureloss AP due to drawing and an entire length (L1+L2) of a pipe-drawnportion, in Example 2 of the present invention;

FIG. 5 is a sectional view showing one example of a conventionalterminal structure of a high-pressure fuel pipe for a directioninjection engine; and

FIG. 6 is a sectional view showing one example of a terminal structureof an eye joint used in a conventional terminal structure of ahigh-pressure fuel pipe for a direction injection engine in a partiallybroken fashion.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

In the present invention, a fuel pipe 1, 11 is composed of a steel pipeor a stainless steel pipe made of carbon steel for a high-pressure pipeor austenite stainless steel or the like which has been cut to apredetermined size and having an outer diameter D in a range from Φ6 mmto Φ10 mm and t/D (t: thickness, D: pipe outer diameter) in a range from0.1 to 0.2. Further, as such steel pipe made of carbon steel for ahigh-pressure pipe or such stainless steel pipe made of austenitestainless steel, an electric-resistance welded steel pipe, asemi-seamless pipe, a seamless pipe, or the like can be used.Incidentally, when the steel pipe made of carbon steel is used, Ni, Zn,Sn or an alloy based upon these metals is generally provided on an innerface and/or an outer face of the steel pipe for corrosion protection.

As shown in FIG. 1 and FIG. 2, a connection head 2, 12 in a terminalstructure of a high-pressure fuel pipe for a direct injection engineaccording to the present invention has a spherical, curved-face orconical pressing seat face 2-1, 12-1 at an end of the connection head onthe connection side, a nut pressure-receiving face 2-2, 12-2 continuedto the pressing seat face 2-1, 12-1, and a fuel pipe insertion portion(hakama) 2-3, 12-3 continued to the nut pressure-receiving face 2-2,12-2 which are obtained by plastic working or cutting work.

The terminal structure of a high-pressure fuel pipe for a directinjection engine according to the present invention shown in FIG. 1 ischaracterized by having a constituent feature that a straight pipeportion 1-1 a is provided at a first-stage drawn portion 1-1 formed atthe end of the fuel pipe continued to the fuel pipe insertion portion2-3 of the connection head 2 by press forming.

Particularly, the terminal structure of the present invention ischaracterized in that an outer diameter D1 of the first-stage drawnportion 1-1 relative to a fuel pipe diameter D satisfies 0.8≦D1≦0.9 D; alength L1 of the drawn portion 1-1 having the outer diameter D1 in anaxial direction of the pipe from an end of the fuel pipe insertionportion 2-3 has a straight pipe portion 1-1 a satisfying L1≧0.06 D ; alinear length L2 in the axial direction of the pipe from a terminal endof the straight pipe portion 1-1 a on the opposite side to theconnection head 2, to a drawing-work terminal end, is 0.14 D or more;and an entire length (L1+L2) of the first-stage drawn portion 1-1 is 1.5D or less.

Here, the reason why the length L1 of the first-stage drawn portion 1-1in the axial direction is determined to be 0.06 D or more is becausewhen the length L1 is less than 0.06 D, stress is concentrated on abrazed portion. Further, the reason why the entire length (L1+L2) of thefirst-stage drawn portion 1-1 is limited to 1.5 D or less is becausewhen the entire length (L1+L2) exceeds 1.5 D, pressure loss of two ormore times that in the case that the drawing work has not be performedoccurs.

An angle θ1 of a first-stage tapered pipe portion 1-1 b can be setappropriately according to the entire length (L1+L2) of the first-stagedrawn portion 1-1.

According to a terminal structure of a high-pressure fuel pipe for adirect injection engine of the present invention shown in FIG. 1, theouter diameter D1 of the first-stage drawn portion 1-1 formed at thepipe end by press working to a fuel pipe diameter D satisfies 0.8≦D1≦0.9D; a connection head 2 is fitted on the end of the fuel pipe 1; and thefitted portion is brazed, the connection head 2 having the spherical,curved-face or conical pressing seat face 2-1 at the connection-side endof the connection head, a nut pressure-receiving face 2-2 continued tothe pressing seat face 2-1, and a fuel pipe insertion portion (hakama)2-3 continued to the nut pressure-receiving face 2-2 which are formed byplastic working or cutting work, and the end of the fuel pipe 1 beingprovided with the first-stage drawn portion 1-1 having the straight pipeportion 1-1 a satisfying the condition that the length L1 of thefirst-stage drawn portion 1-1 having the outer diameter D1 in thepipe-axial direction from the end of the fuel pipe insertion portion isL1≧0.06 D.

The case of the above-described terminal structure of a high-pressurefuel pipe for a direct injection engine shown in FIG. 1 can preventstress concentration to the brazed portion between the fuel pipe 1 andthe connection head 2 effectively by working of the straight pipeportion 1-1 a satisfying the condition that the length L1 of thefirst-stage drawn portion 1-1 having the outer diameter D1 in thepipe-axial direction from the end of the fuel pipe insertion portionsatisfies L1≧0.06 D.

Further, the terminal structure of a high-pressure fuel pipe for adirect injection engine of the present invention shown in FIG. 2 ischaracterized by having a constituent feature that a drawn portion isformed on the end of the fuel pipe continued to the fuel pipe insertionportion 2-3 of the connection head 2 in a two-stage fashion.Particularly, the present invention is a terminal structure where anouter diameter D1 of a first-stage drawn portion 11-1 to a fuel pipediameter D satisfies 0.8≦D1≦0.9 D; a connection head 12 is fitted on theend of the fuel pipe 11; and the fitted portion is brazed, theconnection head 12 having the spherical, curved-face or conical pressingseat face 12-1 at the connection-side end of the connection head, thenut pressure-receiving face 12-2 continued to the pressing seat face12-1, and the fuel pipe insertion portion (hakama) 12-3 continued to thenut pressure-receiving face 12-2 which are formed by plastic working orcutting work, and the end of the fuel pipe 1 being provided with thefirst-stage drawn portion 11-1 having a straight pipe portion 11-lasatisfying the condition where a length L1 of the first-stage drawnportion 1-1 having the diameter D1 in a pipe-axial direction from theend of the fuel pipe insertion portion satisfies L1≧0.06 D and asecond-stage drawn portion 11-2 continued to the first-stage drawnportion 11-1 and having a straight pipe portion 11-2 a having an outerdiameter D2 larger than the outer diameter D1 of the first-stage drawnportion 11-1.

Even in the case of the terminal structure of a high-pressure fuel pipefor a direct injection engine where the drawn portion have been formedin the fuel pipe end in a two-staged fashion, shown in FIG. 2,respective angles θ2, θ3 of a first-stage tapered pipe portion 11-1 band a second-stage tapered pipe portion 11-2 b in a linear length L2 inthe pipe-axial direction including the second-stage drawn portion 11-2from an end of the first-stage straight pipe portion 11-1 a on theopposite side to the connection head 12 to a drawing termination end,corresponding to the linear length L2 in the pipe-axial direction fromthe terminal end, opposite to the connection head 2, of the straightpipe portion 1-1 a of the terminal structure shown in FIG. 1 to adrawing termination end can be set appropriately in response to theentire length (L1+L2) of the drawn portion 11-1.

In the case of the terminal structure of a high-pressure fuel pipe for adirect injection engine shown in FIG. 2, in the terminal structure wherethe outer diameter D1 to the fuel pipe diameter D satisfies 0.8≦D1≦0.9D, stress concentration to the brazed portion with the connection head12 can be not only prevented effectively by working of the first-stagedrawn portion 11-1 having the straight pipe portion 11-1 a satisfyingthe condition where the length L1 of the first-stage drawn portion 11-1having the outer diameter D1 in the pipe-axial direction from the end ofthe fuel pipe insertion portion is L1≧0.06 D but also an dispersioneffect of stress acting on the fuel pipe 11 can be obtained by workingof the second-stage drawing portion 11-2, so that even if a load(displacement) in a bending direction to the high-pressure fuel pipe 11occurs, stress concentration is avoided and a problem of damage of thefuel pipe 11 is almost all solved.

EXAMPLES

The present invention will be specifically described below based uponExamples. However, the present invention is not restricted by thefollowing Examples and it can be modified in design arbitrarily withinthe scope of the gist of the present invention.

Example 1

A terminal structure of a high-pressure fuel pipe for a direct injectionengine shown in FIG. 1 was manufactured and a reduction effect of stressconcentration to a brazed portion between a fuel pipe and a connectionhead was examined.

In this Example, a stainless steel pipe made of austenitic stainlesssteel and having an outer diameter D of Φ8 mm and t/D (t: thickness, D:pipe outer diameter) of 0.15 was used as the fuel pipe, and a connectionhead made of stainless steel and having a conical pressing seat face atthe connection-side end of the connection head, a nutpressure-receiving. face continued to the pressing seat face, and a fuelpipe insertion portion (brazing length M=7 mm) continued to the nutpressure-receiving face which were obtained by plastic working wasbrazed to an end of the fuel pipe 1 having a first-stage drawn portionhaving D1=7 mm (constant) , L1=0 to 4 mm, and an outer diameter ratio=0to 0.5. A bending stress, L1, and the outer diameter in this Example areshown in Table 1 and a relationship between the bending stress and theouter diameter ratio is shown in FIG. 3.

From data shown in Table 1 and FIG. 3, it is understood that a change ofthe bending stress is made small by providing the straight pipe portionsatisfying the condition where the length L1 of the first-stage drawnportion having the outer diameter D1 in the pipe-axial direction fromthe fuel pipe insertion portion terminal satisfies L1≧0.06 D. Thisresult supports that when the straight pipe portion satisfying thecondition of L1≧0.06 D is provided in the first-stage drawn portion,stress concentration to the brazed portion between the fuel pipe and theconnection head can be prevented effectively.

TABLE 1 L1 Outer Diameter Bending Stress (mm) Ratio (MPa) Comparative 00 214.22 Example 0.25 0.03 223.82 Present 0.5 0.06 176.13 Invention 10.13 175.68 2 0.25 168.61 3 0.38 167.82 4 0.50 159.39

Example 2

A terminal structure of a high-pressure fuel pipe for a direct injectionengine shown in FIG. 1 and similar to Example 1 was manufactured and achange of pressure loss due to drawing length (L1+L2) was examined.

In this Example, a stainless steel pipe made of austenitic stainlesssteel material was used as the fuel pipe 1, and a connection head madeof stainless steel and having a conical pressing seat face at theconnection-side end of the connection head, a nut pressure-receivingface continued to the pressing seat face, and a fuel pipe insertionportion (brazing length M=7 mm) continued to the nut pressure-receivingface which were obtained by plastic working was brazed to an end of afuel pipe 1 having a first-stage drawn portion where the outer diameterD and the outer diameter D1 of the straight pipe portion of thefirst-stage drawn portion are D=Φ6.0 to Φ10.0 mm and D1=4.8 to 8.0 mm,respectively. A relationship between increase of pressure loss ΔP andthe entire length (L1+L2) of the pipe-drawn portion is shown in FIG. 4.

As is apparent from data shown in FIG. 4, when the drawing length(L1+L2) is determined based upon that the increase of pressure loss dueto drawing the pipe end of the fuel pipe is 100% or less (double inloss) according to calculation of the pressure loss ΔP, (L1+L2)≦1/5 D isobtained. Accordingly, the entire length (L1+L2) of the first-stagedrawn portion 1-1 was determined as 1.5 D or less in the presentinvention.

Example 3

A terminal structure (two-stage drawing) of a high-pressure fuel pipefor a direct injection engine shown in FIG. 2 was manufactured and areduction effect of stress concentration to a brazed portion between afuel pipe and a connection head was examined.

In this Example, a stainless steel pipe made of austenitic stainlesssteel and having an outer diameter D of Φ8 mm and t/D (t: thickness, D:pipe outer diameter) of 0.15 was used as the fuel pipe, and a connectionhead made of stainless steel and having a conical pressing seat face atthe connection-side end of the connection head, a nut pressure-receivingface continued to the pressing seat face, and a fuel pipe insertionportion (brazing length M=7 mm) continued to the nut pressure-receivingface which were obtained by plastic working was brazed to an end of afuel pipe having a two-stage drawn portion with D1=7 mm, D2=7.5 mm, L1=1mm, and L2=6 mm in the same manner as Examples 1 and 2.

As the result of examination of the reduction effect of the stressconcentration corresponding to the brazed portion between the fuel pipeand the connection head to the terminal structure manufactured, it hasbeen found that a dispersion effect of stress acting on the fuel pipe isobtained by working of the second-stage drawn portion in addition toworking of the first-stage drawn portion, so that even if a load(displacement) in a bending direction to the high-pressure fuel pipeoccurs, stress concentration can be avoided.

The present invention can prevent stress concentration to a brazedportion with a connection head effectively by, in a terminal structureof a high-pressure fuel pipe for a direct injection engine where aconnection head having a spherical or a curved-face pressing seat faceat a distal end thereof and a fuel pipe insertion portion on an oppositeside of the pressing seat face is brazed to an end of a fuel pipecomposed of a steel pipe or a stainless steel pipe, providing aone-stage drawn portion having a straight pipe portion satisfying aspecific condition at an end of a fuel pipe continued to the fuel pipeinsertion portion of the connection head, and a dispersion effect ofstress acting on a fuel pipe can be further obtained by providing asecond-stage drawn portion continued to the one-stage drawn portion, sothat even if a load (displacement) in a bending direction to thehigh-pressure fuel pipe occurs, stress concentration is avoided, andlarge contribution to reduction of risk of a fuel pipe for a directinjection engine is obtained.

REFERENCE SIGNS LIST

-   -   1, 11 . . . high-pressure fuel pipe,    -   1-1, 11-1 . . . first-stage drawn portion    -   1-1 a, 11-1 a, 11-2 a . . . straight pipe portion    -   1-1 b, 11-1 b, 11-2 b . . . tapered pipe portion    -   2, 12 . . . connection head    -   2-1, 12-1 . . . pressing seat face    -   2-2, 12-2 . . . nut-pressure receiving face,    -   2-3, 12-3 . . . fuel pipe insertion portion (hakama)    -   11-2 . . . second-stage drawn portion    -   θ1, θ2, θ3 . . . angle of tapered pipe portion

What is claim is:
 1. A terminal structure of a high-pressure fuel pipe for a direct injection engine, comprising a connection head brazed to an end of a steel or stainless steel fuel pipe, the connection head having a spherical or a curved-face pressing seat face at a distal end thereof and a fuel pipe insertion portion on an end opposite of the pressing seat face, wherein the end of the fuel pipe continued from the fuel pipe insertion portion of the connection head has a two-stage drawn portion, an outer diameter D1 of a first-stage drawn portion located on the side of the connection head, relative to a fuel pipe diameter D, satisfying 0.8≦D1≦0.9 D, wherein a length L1 of the first-stage drawn portion having the outer diameter D1 from an end of the fuel pipe insertion portion in an axial direction of the pipe satisfies L1≧0.06 D, and wherein a second-stage drawn portion continued from the first-stage drawn portion has a straight pipe portion having an outer diameter D2 larger than the outer diameter D1 of the first-stage drawn portion.
 2. The terminal structure of a high-pressure fuel pipe for a direct injection engine according to claim 1, wherein a linear length L2 in the axial direction of the pipe from a terminal end of the length L1 of the drawn portion having the outer diameter D1 in the axial direction of the pipe, to a drawing-termination end, is 0.14 D or more, and an entire length (L1+L2) of the drawn portion of the pipe is 1.5 D or less. 